Guide vane

Patent metadata

Field	Value
Publication number	US-10012103-B2
Application number	US-201514925149-A
Country	US
Kind code	B2
Filing date	Oct 28, 2015
Priority date	Nov 10, 2014
Publication date	Jul 3, 2018
Grant date	Jul 3, 2018

Abstract

A gas turbine engine variable guide vane has a fixed portion on an upstream side, a movable flap on a downstream side and a transfer slot between a fixed portion trailing surface and a movable flap leading surface. The movable flap has opposite pressure and suction sides along a chord line between leading and trailing edges, and is rotatable about an axis along a movable flap span over a range of angular positions between open and closed. The trailing surface has a substantially U-shaped profile with first and second branches respectively partially around the pressure and suction sides. The transfer slot has inlet and exhaust ports respectively on the pressure and suction sides. In the closed position the suction side contacts the second branch closing the exhaust port, and in the open position the second branch directs a first air flow through the transfer slot tangentially over the suction surface.

First claim

The invention claimed is:

1. A variable guide vane for a gas turbine engine comprising:
a fixed portion arranged on an upstream side;
a movable flap arranged on a downstream side; and
a transfer slot defined between a trailing surface of the fixed portion and a leading surface of the movable flap,
the movable flap having opposite pressure and suction sides extending along a chord line between leading and trailing edges, the movable flap being rotatable about an axis extending along a span of the movable flap over a range of angular positions between open and closed,
the trailing surface having a substantially U-shaped profile with a first branch extending partially around the pressure side of the movable flap, and an opposite second branch extending partially around the suction side of the movable flap,
the transfer slot having an inlet port arranged on the pressure side of the movable flap and an exhaust port arranged on the suction side of the movable flap,
wherein in use, in the open position the suction side abuts the second branch to close the exhaust port, and in the closed position the second branch directs a first air flow passing through the transfer slot tangentially over the suction surface of the movable flap.

2. The variable guide vane as claimed in claim 1 , wherein the fixed portion comprises an internal cavity, the internal cavity being in fluid communication with the transfer slot, the internal cavity being supplied with air at a pressure higher than the airflow passing through the transfer slot, and, in use, directing a second air flow into the transfer slot, directed towards the exhaust port, to thereby supplement the first air flow.

3. The variable guide vane as claimed in claim 2 , wherein the internal cavity is fluidly connected to the transfer slot by a plurality of feed slots, the feed slots being arranged along the span of the movable flap.

4. The variable guide vane as claimed in claim 1 , wherein the transfer slot has a convergent flow path in a direction extending from the pressure side of the movable flap to the suction side of the movable flap.

5. The variable guide vane as claimed in claim 1 , wherein a camber line of the movable flap is coincident with the chord line.

6. The variable guide vane as claimed in claim 1 , wherein the axis of the movable flap is offset from the chord line.

7. The variable guide vane as claimed in claim 6 , wherein the offset of the axis is in a direction extending towards the pressure side of the movable flap.

8. The variable guide vane as claimed in claim 1 , wherein the second branch has an elliptical sectional profile.

9. The variable guide vane as claimed in claim 2 , further comprising a heater adapted to impart heat energy to the second air flow.

10. A gas turbine engine comprising a variable guide vane as claimed in claim 1 .

Assignees

• Rolls Royce Plc

Inventors

• Pachidis Vasileios
• Soria Carlos

Classifications

• F01D25/10

  Heating, e.g. warming-up before starting · CPC title

• F04D29/684

  by fluid injection · CPC title

• F05D2250/75

  given by its similarity to a letter, e.g. T-shaped · CPC title

• F01D17/162

  for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line (F01D17/167 takes precedence) · CPC title

• F01D5/146 Primary

  of blades with tandem configuration, split blades or slotted blades · CPC title